On the feasible development of gimballess control systems for launch vehicles using GPS satellite navigation equipment

Рубрика: 
1Degtyarev, АV, 2Degtyarev, MA, 1Davydenko, SA, 2Makarov, AL, 3Snegirev, MG, 2Sirenko, VN, 3Tikhonov, VL, 1Shekhovtsov, VS
1Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
2Yangel Yuzhnoye State Design Office, Dnipro, Ukraine
3Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 2015, 21 ;(6):03–12
https://doi.org/10.15407/knit2015.06.003
Язык публикации: Russian
Аннотация: 

We present results on the feasibility of developing the Gimballess Navigation Inertial Satellite Control System (NISCS/ GPS SNE) on the basis of MEMMS-sensors and GPS Satellite Navigation Equipment (GPS SNE) for commercial Launch Vehicles (LV) of light and middle classes. We note that this NISCS/GPS SNE is of less cost, less mass, less dimensions, and energy capacity. Feasibility of developing the NISCS/ GPS SNE is based on the analysis of solution of two tasks: a) statistic model ling of LV disturbed motion, which takes into account the errors of NISCS/GPS SNE operation, and b) establishment of the NISCS/GPS SNE rational structure and instruments, which takes the modeling and experimental development results into account. We demonstrate that NISCS/ GPS SNE use will be helping to increase competitiveness of Launch Vehicle of a reviewed class due to the reduction of LV launch cost and increase of Payload mass. 

Ключевые слова: GPS satellite navigation equipment, hybrid Control System, MEMMS gyroscopes and accelerometers, unmanned navigation system, weakly connected system.
References: 

1. Degtyarev A.V. Scientific and methodological bases of missile systems modernization. Doctor’s thesis. 245 p. (Yuzhnoye Design Office, Dnepropetrovsk, 2012) [in Russian].

2. Degtyarev A. V., Kushnarev A. P., Makarov A. L. et al. Analiz vozmozhnosti razrabotki v GP «KB «Juzhnoe» integrirovannoj inercial'no-sputnikovoj navigacionnoj sistemy s chuvstvitel'nymi jelementami, ispol'zujushhimi razlichnye fizicheskie principy, v tom chisle i vypolnennye po MJeMS-tehnologii, dlja perspektivnyh obrazcov raketno-kosmicheskoj tehniki: (Tehn. otchet). No. 21.17966.159 OT. 243 p. (Yuzhnoye Design Office, Dnepropetrovsk, 2015) [in Russian].

3. Kirichenko A. F., Ignat'ev V. G., Salenko D. V., Stadnik N. V. RV "Cyclone-4". Navigation algorithms. NTO AARG. 371111. 029 90 103. (NPP «Hartron-Arkos», Kharkov, 2011) [in Russian].

4. Kirichenko A. F., Luk'janovich A. E., Ostapenko V. M. RV "Mayak-22". Navigation system, guidance and stabilization. Jeskiznyj proekt. Ch. 3. (NPP «Hartron-Arkos», Kharkov, 2013) [in Russian].

5. Sirenko V. N. , Snegirev M. G. Issledovanie vozmozhnosti postroenija SU pri ispol'zovanii KKP s povyshennymi pogreshnostjami i informacii pod AP-SNS NTO, 53 p. (Yuzhnoye Design Office, Dnepropetrovsk, 2015) [in Russian].

6. Jeffrey A. G. Characterization, control and compensation of MEMS rate and rate-integrating gyroscopes: A doctor of philosophy (Electrical Engineering) dissertation. 182 p. (The University of Michigan, 2012).

7. Guochang Xu. GPS. Theory, algorithms and applications, 351 p. (Springer-Verlag, Heidelberg, 2007).

8. Quinchia A. G., Falco G., Falletti E., et al. A comparison between different error modeling of MEMS applied to GPS/INS integrated systems. Sensors. 13, 9549—9588 (2013).
https://doi.org/10.3390/s130809549

9. Sveinsson A. INS/GPS error analysis and integration. 114 p. (Reyjavik University, 2012).